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gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200225153233)

Failing for the past 1 build (Since Failed #318 )
Took 14 sec.

Error Message

cost contains unsolved variables [Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[4,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[1,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[4,0], Mission2.FlightState.Relax2.R[4,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[1,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[2,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[2,0], Mission2.Aircraft.Fuselage.Relax2.n_{pass}[0], Mission2.FlightState.Relax2.R[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[0,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[1,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[0,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[2,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[1,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[4,0], Mission2.FlightState.Relax2.R[0,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[4,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[3,0], Mission2.FlightState.Relax2.\gamma[2,0], Mission2.FlightState.Relax2.\gamma[0,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[2,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[3,0], Mission2.FlightState.Relax2.\gamma[4,0], Mission2.FlightState.Relax2.R[3,0], Mission2.FlightState.Relax2.R[1,0], Mission2.FlightState.Atmosphere.Relax2.T_s[4,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[1,0], Mission2.FlightState.Relax2.\gamma[1,0], Mission2.FlightState.Atmosphere.Relax2.C_1[4,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[0,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[4,0], Mission2.FlightState.Atmosphere.Relax2.T_s[1,0], Mission2.FlightState.Atmosphere.Relax2.T_s[3,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[3,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[1,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[0,0], Mission2.FlightState.Atmosphere.Relax2.C_1[0,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[3,0], Mission2.FlightState.Atmosphere.Relax2.C_1[1,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[0,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[4,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[3,0], Mission2.FlightState.Atmosphere.Relax2.T_s[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[0,0], Mission2.FlightState.Atmosphere.Relax2.C_1[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[4,0], Mission2.FlightState.Atmosphere.Relax2.C_1[3,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[1,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[1,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[0,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[0,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[3,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[3,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[0,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[2,0], Mission2.FlightState.Relax2.\gamma[3,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[2,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[3,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[1,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[3,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[0,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[1,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[2,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[2,0], Mission2.FlightState.Atmosphere.Relax2.T_s[0,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[3,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[1,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[3,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[0,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[2,0]]

Stacktrace

Traceback (most recent call last):
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
    testfn(name, import_dict, path)(self)
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn
    mod.test()
  File "SPaircraft.py", line 89, in test
    sol = optimize_aircraft(m, substitutions, fixedBPR, pRatOpt, mutategparg)
  File "SPaircraft.py", line 65, in optimize_aircraft
    sol = m_relax.localsolve(verbosity=2, iteration_limit=200, reltol=0.01, mutategp=mutategparg)#, x0 = x0)
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/constraints/prog_factories.py", line 124, in solvefn
    result = progsolve(solver, verbosity, **kwargs)
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/constraints/sgp.py", line 169, in localsolve
    self.result = gp.generate_result(solver_out, verbosity)
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/constraints/gp.py", line 211, in generate_result
    result = self._compile_result(solver_out)  # NOTE: SIDE EFFECTS
  File "/Users/jenkins/workspace/CE_RM_SPaircraft_PR/mosek/gpkit/gpkit/constraints/gp.py", line 298, in _compile_result
    % cost.varkeys.keys())
ValueError: cost contains unsolved variables [Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[4,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[1,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[4,0], Mission2.FlightState.Relax2.R[4,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[1,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[2,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[2,0], Mission2.Aircraft.Fuselage.Relax2.n_{pass}[0], Mission2.FlightState.Relax2.R[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[0,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[1,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[0,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[2,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[1,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[4,0], Mission2.FlightState.Relax2.R[0,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[4,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[3,0], Mission2.FlightState.Relax2.\gamma[2,0], Mission2.FlightState.Relax2.\gamma[0,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[2,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[3,0], Mission2.FlightState.Relax2.\gamma[4,0], Mission2.FlightState.Relax2.R[3,0], Mission2.FlightState.Relax2.R[1,0], Mission2.FlightState.Atmosphere.Relax2.T_s[4,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[1,0], Mission2.FlightState.Relax2.\gamma[1,0], Mission2.FlightState.Atmosphere.Relax2.C_1[4,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[0,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[4,0], Mission2.FlightState.Atmosphere.Relax2.T_s[1,0], Mission2.FlightState.Atmosphere.Relax2.T_s[3,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[3,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[1,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[0,0], Mission2.FlightState.Atmosphere.Relax2.C_1[0,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[3,0], Mission2.FlightState.Atmosphere.Relax2.C_1[1,0], Mission2.FlightState.Atmosphere.Relax2.L_{atm}[0,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[4,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[3,0], Mission2.FlightState.Atmosphere.Relax2.T_s[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[0,0], Mission2.FlightState.Atmosphere.Relax2.C_1[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[4,0], Mission2.FlightState.Atmosphere.Relax2.C_1[3,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[1,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[1,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[0,0], Mission2.FlightSegment.FlightP.Relax2.RC_{min}[0,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[3,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{t}}[3,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[0,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[2,0], Mission2.FlightState.Relax2.\gamma[3,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[2,0], Mission2.FlightState.Atmosphere.Relax2.M_{atm}[3,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[1,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[4,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[2,0], Mission2.FlightSegment.FlightP.AircraftP.WingPerformance.Relax2.f_{L_{o}}[3,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[0,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.W_{Load_{max}}[1,0], Mission2.FlightState.Atmosphere.Relax2.T_{sl}[2,0], Mission2.FlightState.Atmosphere.Relax2.p_{sl}[2,0], Mission2.FlightState.Atmosphere.Relax2.T_s[0,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[3,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[1,0], Mission2.FlightSegment.FlightP.AircraftP.Relax2.V_{stall}[3,0], Mission2.FlightState.Atmosphere.Relax2.R_{atm}[0,0], Mission2.Aircraft.Engine.EnginePerformance.CombustorPerformance.Relax2.M_{4a}[2,0]]

Standard Output

Beginning signomial solve.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.337 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.272 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.323 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.312 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.302 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.253 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.304 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.325 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.332 seconds.
Solving took 9 GP solves and 11.7 seconds.
Checking for relaxed constants...
GP iteration 0 has relaxed constants

Cost
----
 2.72e+110

Free Variables
--------------
                   | Mission.Aircraft.Engine.Turbine.Relax
        C_{p_{t2}} : 2.246                                                Cp Value for Combustion Products in LP Turbine

                   | Mission.Aircraft.Fuselage.Relax
          l_{nose} : 1.067                                                Nose length
          n_{pass} : [ 2.86     ]                                         Number of passengers

                   | Mission.Aircraft.Relax
f_{L_{total/wing}} : 1.683                                                Total lift as a percentage of wing lift

                   | Mission.Aircraft.Wing.WingNoStruct.Relax
     \tan(\Lambda) : 1.109                                                Tangent of quarter-chord sweep angle

                   | Mission.FlightState.Atmosphere.Relax
           L_{atm} : [ 1.78      1         1         1         1        ] Temperature lapse rate
            T_{sl} : [ 1         1         1.27      1         1        ] Temperature at sea level

                   | Mission.Relax
           R_{req} : 2.352                                                Required Cruise Range

GP iteration 1 has relaxed constants

Cost
----
 1.472e+75

Free Variables
--------------
          | Mission.Aircraft.Engine.Combustor.Relax
hold_{4a} : 1.117        1+(gamma-1)/2 * M_4a**2

          | Mission.Aircraft.Fuselage.Relax
 n_{pass} : [ 1.04     ] Number of passengers

          | Mission.Aircraft.LandingGear.Relax
 h_{hold} : 1.007        Hold height

Solution check warning: Primal solution computed cost did not match solver-returned cost: 1.998972324382873e+72 vs 1.99908047491e+72
WEIGHT DIFFERENCES


Total Fuel Weight Percent Diff: [-92.97033935]


Total Aircraft Weight Percent Diff: [-21.17214269]


Engine Weight Percent Diff: -58.76555047012018


Fuselage Weight Percent Diff: 2.3096728084332754


Payload Weight Percent Diff: [-0.04003555]


VT Weight Percent Diff: -8.68091963167528


HT Weight Percent Diff: -93.22548823252279


Wing Weight Percent Diff: 8.05615841282999




WING DIFFERENCES


Wing Span Percent Diff: -0.029994309491006375


Wing Area Percent Diff: 33.877703222109




HORIZONTAL TAIL DIFFERENCES


HT Area Percent Diff: 41.32273730746586




VERTICAL TAIL DIFFERENCES




VT Span Percent Diff: -11.04613420758646


VT Area Percent Diff: -60.40801894574819




CRUISE SEGMENT 1 DRAG DIFFERENCES


Overall Cd Percent Diff: [-19.04555051]


L/D Percent Diff: [24.03457236]


Nacelle Cd Percent Diff: [-94.59139722]


HT Cd Percent Diff: [-80.83177273] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-58.32239675] dimensionless


Wing Cd percent Diff: [-14.78360717]
Induced Drag Cd Percent Diff: [0.72572723]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-90.67468512]




FUSELAGE DIFFERENCES




Weight of HB material: -39.327543722714886 


Weight of VB material: 90.50191622839411 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.69501812]
Beginning signomial solve.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.45 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.24 seconds.
Using solver 'mosek'
Solving for 1749 variables.
Solving took 0.324 seconds.
Beginning signomial solve.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.245 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.244 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.249 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.225 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.24 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.234 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.22 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.212 seconds.
Using solver 'mosek_conif'
Solving for 1749 variables.
Solving took 0.229 seconds.

Standard Error